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Evaluation of the influence of radiation on a GH2/GO2 rocket combustor 会议论文
AIAA Propulsion & Energy Forum, VIRTUAL EVENT, 2020-08-17
Authors:  Li B(李波);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1358Kb)  |  Favorite  |  View/Download：158/49  |  Submit date：2021/02/01
Ventilated partial cavitating flow around a blunt body near the free surface 会议论文
16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2016, Honolulu, HI, United states, April 10, 2016 - April 15, 2016
Authors:  Wang YW(王一伟);  Wu XC(吴小翠);  Huang CG(黄晨光)
View  |  Adobe PDF(757Kb)  |  Favorite  |  View/Download：190/40  |  Submit date：2019/11/20
Axisymmetric bodies  Cavity boundaries  Free surfaces  High  speed underwater vehicles  Launching systems  Media properties  Unsteady behaviors  Ventilated cavitation  
Optimization of the self-condensing CO2 transcritical power cycle using solar thermal energy 会议论文
10th International Conference on Applied Energy (ICAE), Hong Kong, HONG KONG, AUG 22-25, 2018
Authors:  Pan LS(潘利生);  Li,Bing;  Shi,Weixiu;  Wei XL(魏小林)
Adobe PDF(1140Kb)  |  Favorite  |  View/Download：118/38  |  Submit date：2022/11/24
CO2 transcritical power cycle  Supercritical CO2 Brayton cycle  Solar thermal energy  CO2 condensation  
Downstream pressure variation induced hysteresis in the scramjet isolator 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH;  Jia YN(贾轶南);  Zhang XY(张新宇);  Yue, Lianjie(yuelj@imech.ac.cn)
View  |  Adobe PDF(704Kb)  |  Favorite  |  View/Download：273/93  |  Submit date：2018/01/16
Spacecraft  
Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Li GL(李广利);  Cui K(崔凯);  Xiao Y(肖尧);  Xu YZ(徐应洲)
Adobe PDF(664Kb)  |  Favorite  |  View/Download：397/96  |  Submit date：2018/01/16
Aerodynamics  Angle Of Attack  Angle Of Attack Indicators  Boundary Layers  Drag  Drag Coefficient  High Pressure Effects  Hypersonic Aerodynamics  Hypersonic Flow  Spacecraft  
Comparison of drag prediction using RANS models and DDES for the DLR-F6 configuration using high order schemes 会议论文
54th AIAA Aerospace Sciences Meeting, 2016, San Diego, CA, United states, January 4, 2016 - January 8, 2016
Authors:  Gan JY;  Shen YQ(申义庆);  Zha GC
Adobe PDF(555Kb)  |  Favorite  |  View/Download：292/94  |  Submit date：2017/05/05
Central Differencing  Drag Prediction  Finite Difference Scheme  High  Order Scheme  Line Relaxation  Mesh Refinement  Trailing Edges  Turbulent Models  
Oscillation-free adaptive simulation of compressible two-fluid flows with different types of equation of state 会议论文
8th Workshop on Synthetic Turbulence Models, Paris, FRANCE, JUN 28-29, 2012
Authors:  Zheng HW(郑洪伟);  Shu C;  Chew YT;  Qin N;  Zheng HW(郑洪伟)
Adobe PDF(972Kb)  |  Favorite  |  View/Download：908/283  |  Submit date：2013/03/01
Compressible Multifluids  Adaptive  Equation Of State  
Quaso-1D Compressible Flow of Hydrocarbon Fuel 会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Atlanta, Georgia., July 30-Augest 1, 2012
Authors:  Cheng D(程迪) and Fan XJ(范学军)
Adobe PDF(911Kb)  |  Favorite  |  View/Download：724/251  |  Submit date：2013/03/05
Quasi-1D compressible flow of hydrocarbon fuel 会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United states, JUL 30-AUG 01, 2012
Authors:  Cheng D(程迪);  Fan XJ(范学军);  Yang M(杨猛);  Cheng D(程迪)
Adobe PDF(1018Kb)  |  Favorite  |  View/Download：537/152  |  Submit date：2014/02/24
DNS of shock/boundary layer interaction flow in a supersonic compression ramp 会议论文
6th International Conference on Computational Fluid Dynamics, St Petersburg, RUSSIA, JUL 12-16, 2010
Authors:  Li XL(李新亮);  Fu DX(傅德薰);  Ma YW(马延文);  Liang X(梁贤);  Li, XL (reprint author), CAS, Inst Mech, LHD, Beijing 100190, Peoples R China
Adobe PDF(966Kb)  |  Favorite  |  View/Download：711/181  |  Submit date：2013/02/26
Turbulent-boundary-layer  Direct Numerical-simulation